View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53078U 26145.37349931 +.00000000 +00000-0 -55520-4 0 00005
2 53078 97.4491 325.3699 0001179 138.0215 222.1103 15.05655168 07
| Epoch (UTC): | 25 May 2026 08:57:50 |
| Eccentricity: | 0.0001179 |
| inclination: | 97.4491° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.3699° |
| argument of perigee: | 138.0215° |
| revolutions per day: | 15.05655168 |
| mean anomaly at epoch: | 222.1103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|